STARLINK-31972, 59923
Orbit data source: Space-Track
STARLINK-31972, 59923 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 Jun 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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59923 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31972
1 59923U 24106B 26080.93002211 .00002892 00000-0 11455-3 0 9995
2 59923 42.9995 263.4971 0001088 266.2429 93.8298 15.27589011102447Epoch: 2026-03-21T22:19Z
TLE epoch observation values (Epoch: 2026-03-21T22:19:13.910Z)
Latitude
-0.00003°
Longitude
109.24544°
Altitude
482.847 km
Speed
7.626 km/s
True Right ascension
17h 33m 59s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:35:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.714 km
Perigee altitude
484.221 km
Semi-major axis
6,863.104 km
Eccentricity
0.00011
Inclination
42.9995°
RAAN
263.4971°
Arg. of periapsis
266.2429°
True anomaly
93.84224°
Mean anomaly
93.8298°
Eccentric anomaly
93.83602°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.00011455
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Other satellites on launch #106 in the year 2024 (2024-06-01 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-31972 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-23 15:21:31.003Z | 223.868° SW | 2026-03-23 15:23:31.003Z | 161.935° S | 38.92° | 2026-03-23 15:26:31.003Z | 79.984° E |
| 5 mins | 2026-03-23 17:00:31.003Z | 279.666° WNW | 2026-03-23 17:02:31.003Z | 345.397° N | 40.11° | 2026-03-23 17:05:31.003Z | 68.904° E |
| 5 mins | 2026-03-23 18:39:31.003Z | 294.692° NW | 2026-03-23 18:41:31.003Z | 344.717° N | 40.071° | 2026-03-23 18:44:31.003Z | 87.027° E |
| 5 mins | 2026-03-23 20:18:31.003Z | 273.47° WNW | 2026-03-23 20:20:31.003Z | 220.47° SW | 36.515° | 2026-03-23 20:23:31.003Z | 135.711° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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